[fltsim.0]
title=Sikorsky S-39CS NC52V
sim=SIKORSKY S-39CS NC52V
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Sikorsky
ui_type=S-39CS "Amphibion" NC52V
ui_variation="Spirit of Africa" Giraffe spots
description=Single-engined amphibian, used by Martin and Osa Johnson in 1930's on explorations of Africa and Borneo. \n\n
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[forcefeedback]
gear_bump_nose_magnitude=3000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=3000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=3000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=1750
ground_bumps_angle1=8900
ground_bumps_intercept1=5#
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1#
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[General]
performance=Maximum Speed\t120 kts\nCruise Speed\t100 kts\nMaximum Range\t400 nm\nService Ceiling\t18,000 ft\nMax Gross Weight\t4,000 lb\nSeating\t\t4\nUseful Load\t1,322 lb\n\n\n
atc_type=
atc_model=

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0= 170.000, 0.000, 0.000, -2.000
empty_weight= 3150.000
empty_weight_roll_MOI= 3872.000
empty_weight_pitch_MOI= 3385.000
empty_weight_yaw_MOI= 6135.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 4000.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
LeftMain= -0.250, -2.100, 2.500, 32.500, 0.000
RightMain= -0.250, 2.100, 2.500, 32.500, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 350.000
wing_span= 52.000
wing_root_chord= 7.083
wing_dihedral= 1.500
wing_incidence= 0.000
wing_twist= 0.000
oswald_efficiency_factor= 0.686
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.830
wing_pos_apex_vert= 2.500
htail_area= 39.000
htail_span= 16.000
htail_pos_lon= -19.000
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 18.000
vtail_span= 4.837
vtail_sweep= 0.000
vtail_pos_lon= -19.000
vtail_pos_vert= 1.500
elevator_area= 16.610
aileron_area= 18.300
rudder_area= 6.650
elevator_up_limit= 28.000
elevator_down_limit= 20.999
aileron_up_limit= 19.996
aileron_down_limit= 15.000
rudder_limit= 23.995
elevator_trim_limit= 19.498
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[contact_points]
//0  Class
//1  Longitudinal Position        (feet)
//2  Lateral Position             (feet)
//3  Vertical Position            (feet)
//4  Impact Damage Threshold      (Feet Per Minute)
//5  Brake Map                   (0=None, 1=Left, 2=Right)
//6  Wheel Radius                (feet)
//7  Steer Angle                         (degrees)
//8  Static Compression          (feet)  (0 if rigid) 
//9  Max/Static Compression Ratio
//10 Damping Ratio / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//11 Extension Time              (seconds)
//12 Retraction Time             (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at(KIAS)
point.0=1.000,-11.000, 0.000, -4.670, 1600.000, 0.000, 0.520, 30.000, 0.380, 2.500, 1.640, 5.000, 5.000, 1.000, 0.000, 0.000
point.1=1.000, 1.830, -5.000, -6.780, 1600.000, 1.000, 0.520, 0.000, 0.340, 2.500, 1.000, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, 1.830, 5.000, -6.580, 1600.000, 2.000, 0.520, 0.000, 0.340, 2.500, 1.000, 5.000, 5.000, 3.000, 0.000, 0.000

point.4=4.000,-10.000, 0.000, -3.670, 6000.000, 0.000, 0.000, 30.000, 0.450, 2.500, 0.650, 0.000, 0.000, 1.000, 0.000, 0.000
point.5=4.000, 6.000, -2.500, -3.670, 6000.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000
point.6=4.000, 6.000, 2.500, -3.670, 6000.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000
point.7=4.000, 1.250, -8.330, -3.250, 6000.000, 0.000, 0.000, 0.000, 0.750, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000
point.8=4.000, 1.250, 8.330, -3.250, 6000.000, 0.000, 0.000, 0.000, 0.750, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000

point.9=2.000, 0.000, -8.330, -1.500, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.10=2.000, 0.000, 8.330, -1.500, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.11=2.000,-12.170, 0.000, 0.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.12=2.000, 5.000, 0.000, -2.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch=9.000
static_cg_height=6.0

[GeneralEngineData]
engine_type= 0
Engine.0= 2.000, 0.000, 2.50
fuel_flow_scalar= 1.000

[piston_engine]
cylinder_displacement= 109.000
compression_ratio= 8.500
number_of_cylinders= 9
max_rated_rpm= 2400.000
max_rated_hp= 300.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 1
max_design_mp= 40.000
min_design_mp= 0.000
critical_altitude= 8000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
power_scalar=1.000

[propeller]
propeller_type= 1
propeller_diameter= 7.500
propeller_blades= 2
propeller_moi= 8.000
beta_max= 31.800
beta_min= 17.000
min_gov_rpm= 900.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 15.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=1.000

[Reference Speeds]
flaps_up_stall_speed= 54.000
full_flaps_stall_speed= 54.00
cruise_speed= 111.548

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[Views]
eyepoint=0.333210,-0.986815,-0.666421

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=1,0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 3.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 12.666, 0.000
flaps-position.2= 25.332, 0.000
flaps-position.3= 37.999, 0.000